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Sensitivity studies for third-generation gravitational wave observatories
Advanced gravitational wave detectors, currently under construction, are expected to directly observe gravitational wave signals of astrophysical origin. The Einstein Telescope (ET), aExpand
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Scientific objectives of Einstein Telescope
The advanced interferometer network will herald a new era in observational astronomy. There is a very strong science case to go beyond the advanced detector network and build detectors that operateExpand
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Comparison of local plane fitting methods for range data
TLDR
We compare our methods with general least-squares based methods, such as Z-function fitting, the eigenvalue method, the maximum likelihood estimation method, and the renormalization method, an iterative method to obtain the optimal fitting of planes of range data under the noise model. Expand
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Aerodynamic and aeroacoustic simulations of a two-wheel landing gear
Abstract Landing gear noise is one of the dominant noise sources from an aircraft during approach phase due to low engine rate setting. Two different computational fluid dynamics (CFD) codes are usedExpand
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NOISE GENERATION AROUND NACA 0012 WINGTIP USING LARGE-EDDY-SIMULATION
A flow around NACA0012 wingtip is solved using a zonal LES/RANS hybrid method in order to understand the noise generation mechanism around the flap-edge. It is known from the previous studies thatExpand
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INVESTIGATION OF THE FLOW OVER NACELLE / PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION
Aerodynamic performance near maximum lift condition of high-lift configuration commercial aircraft model was improved by a kind of vortex generator “chine” installed on the nacelle in lowspeed windExpand
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Reprint of: Aerodynamic and Aeroacoustic Simulations of a Two-wheel Landing Gear
Abstract Landing gear noise is one of the dominant noise sources from an aircraft during approach phase due to low engine rate setting. Two different computational fluid dynamics (CFD) codes are usedExpand
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Design Exploration of Shielding Effect for Aircraft Engine Noise
TLDR
The multi-objective design exploration of the two-dimensional shielding effect for engine noise using V-tale wing has been performed. Expand
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VALIDATION STUDY OF CFD ANALYSIS FOR HIGH-LIFT SYSTEMS
In this study, three-dimensional flow computations around a simplified three-element high-lift configuration and a realistic high-lift configuration with a nacelle-pylon are performed. By comparisonExpand
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